ATE543730T1 - DEVICE FOR STRAPING AN AIRCRAFT GONDOLA - Google Patents
DEVICE FOR STRAPING AN AIRCRAFT GONDOLAInfo
- Publication number
- ATE543730T1 ATE543730T1 AT09737057T AT09737057T ATE543730T1 AT E543730 T1 ATE543730 T1 AT E543730T1 AT 09737057 T AT09737057 T AT 09737057T AT 09737057 T AT09737057 T AT 09737057T AT E543730 T1 ATE543730 T1 AT E543730T1
- Authority
- AT
- Austria
- Prior art keywords
- cap
- flexible element
- door
- integral
- straping
- Prior art date
Links
- 238000004873 anchoring Methods 0.000 abstract 3
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- Structure Of Belt Conveyors (AREA)
- Shaping Of Tube Ends By Bending Or Straightening (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
Abstract
An aircraft nacelle includes an air intake (12) followed at the upper part by a part (14) integral with the mast, called a cap, and at least one door (16) with a curved profile, and a device for encircling it in the form of at least one flexible element (38), guide elements (40) for allowing the at least one flexible element (38) to follow the curved profile of the at least one door, a first anchoring point (42) of the at least one flexible element (38) integral with a first edge (78) of the cap and another anchoring point of the at least one flexible element (38) integral with a second edge (80) of the cap, whereby the anchoring points (42) allow a relative translational movement, in a direction that is parallel to the longitudinal axis of the nacelle, between the cap (14) and the at least one door (16).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0854892A FR2933956B1 (en) | 2008-07-18 | 2008-07-18 | DEVICE FOR BELTING AN AIRCRAFT NACELLE |
PCT/FR2009/051401 WO2010007311A1 (en) | 2008-07-18 | 2009-07-15 | Device for shrouding an aircraft nacelle |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE543730T1 true ATE543730T1 (en) | 2012-02-15 |
Family
ID=40451242
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT09737057T ATE543730T1 (en) | 2008-07-18 | 2009-07-15 | DEVICE FOR STRAPING AN AIRCRAFT GONDOLA |
Country Status (10)
Country | Link |
---|---|
US (1) | US8757546B2 (en) |
EP (1) | EP2310269B1 (en) |
JP (1) | JP5532448B2 (en) |
CN (1) | CN102131702B (en) |
AT (1) | ATE543730T1 (en) |
BR (1) | BRPI0911008A2 (en) |
CA (1) | CA2731131C (en) |
FR (1) | FR2933956B1 (en) |
RU (1) | RU2496686C2 (en) |
WO (1) | WO2010007311A1 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2966433B1 (en) * | 2010-10-26 | 2012-12-07 | Airbus Operations Sas | AIRCRAFT HOOD INCORPORATING MEANS FOR LIMITING PNEUMATIC ECOPE PHENOMENA |
FR3000721B1 (en) * | 2013-01-09 | 2016-10-14 | Airbus Operations Sas | AIRCRAFT PROPULSIVE ASSEMBLY COMPRISING AERODYNAMIC AERODYNAMIC REAR FITTING FOR SIDEWALLS WITH PROFILED WALLS FOR THE INJECTION OF FRESH AIR ALONG A THERMAL PROTECTION FLOOR |
WO2014151275A1 (en) | 2013-03-15 | 2014-09-25 | United Technologies Corporation | Nacelle mounted latching system |
US10508566B2 (en) * | 2015-03-29 | 2019-12-17 | Rohr, Inc. | Inner fixed structure leading edge latch |
US10618645B2 (en) * | 2015-08-25 | 2020-04-14 | Aerovironment, Inc. | Ganged servo flight control system for an unmanned aerial vehicle |
US11046446B2 (en) | 2017-03-02 | 2021-06-29 | Bell Helicopter Textron Inc. | Tiltrotor aircraft rotating proprotor assembly |
US10994853B2 (en) | 2017-03-02 | 2021-05-04 | Bell Helicopter Textron Inc. | Tiltrotor aircraft rotating proprotor assembly |
FR3063714B1 (en) * | 2017-03-07 | 2019-03-29 | Airbus Operations | AIRCRAFT NACELLE COMPRISING A ROTARY MONTE HOOD AROUND THE LONGITUDINAL AXIS OF THE NACELLE |
US10875627B2 (en) | 2018-05-01 | 2020-12-29 | Bell Helicopter Textron Inc. | Movable cover for a proprotor nacelle |
FR3121429A1 (en) * | 2021-04-02 | 2022-10-07 | Airbus Operations | AIRCRAFT NACELLE COMPRISING A SEAL SYSTEM WITH SPRING FOR A CAP OF SAID NACELLE |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3119581A (en) * | 1960-06-18 | 1964-01-28 | Dunlop Rubber Co | Securing means for inflatable inlet device |
JPS5311760B2 (en) * | 1972-03-18 | 1978-04-24 | ||
US4549708A (en) * | 1982-08-31 | 1985-10-29 | United Technologies Corporation | Cowling latch system |
JP2510444Y2 (en) * | 1989-08-15 | 1996-09-11 | 住友重機械工業株式会社 | Separation device |
US5088775A (en) * | 1990-07-27 | 1992-02-18 | General Electric Company | Seal ring with flanged end portions |
US5350136A (en) * | 1993-05-14 | 1994-09-27 | United Technologies Corporation | Nacelle arrangement |
US6629712B2 (en) * | 2001-03-30 | 2003-10-07 | Hartwell Corporation | Extendable latch |
RU2210523C1 (en) * | 2001-12-14 | 2003-08-20 | Открытое акционерное общество "Авиационный комплекс им. С.В. Ильюшина" | Flying vehicle power-plant pod |
FR2861364B1 (en) * | 2003-10-22 | 2006-02-03 | Airbus France | DEVICE FOR MOUNTING A FITTING BETWEEN AN AIR INLET OF AN AIRCRAFT ENGINE AND A MAT. |
-
2008
- 2008-07-18 FR FR0854892A patent/FR2933956B1/en not_active Expired - Fee Related
-
2009
- 2009-07-15 RU RU2011106025/11A patent/RU2496686C2/en not_active IP Right Cessation
- 2009-07-15 BR BRPI0911008A patent/BRPI0911008A2/en not_active IP Right Cessation
- 2009-07-15 AT AT09737057T patent/ATE543730T1/en active
- 2009-07-15 JP JP2011517974A patent/JP5532448B2/en not_active Expired - Fee Related
- 2009-07-15 CA CA2731131A patent/CA2731131C/en not_active Expired - Fee Related
- 2009-07-15 EP EP09737057A patent/EP2310269B1/en not_active Not-in-force
- 2009-07-15 WO PCT/FR2009/051401 patent/WO2010007311A1/en active Application Filing
- 2009-07-15 US US13/054,290 patent/US8757546B2/en not_active Expired - Fee Related
- 2009-07-15 CN CN200980128903.5A patent/CN102131702B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20110114796A1 (en) | 2011-05-19 |
EP2310269A1 (en) | 2011-04-20 |
JP5532448B2 (en) | 2014-06-25 |
BRPI0911008A2 (en) | 2015-10-06 |
FR2933956B1 (en) | 2010-07-30 |
US8757546B2 (en) | 2014-06-24 |
CN102131702B (en) | 2014-03-19 |
CN102131702A (en) | 2011-07-20 |
CA2731131A1 (en) | 2010-01-21 |
CA2731131C (en) | 2016-09-13 |
JP2011528298A (en) | 2011-11-17 |
WO2010007311A1 (en) | 2010-01-21 |
RU2496686C2 (en) | 2013-10-27 |
EP2310269B1 (en) | 2012-02-01 |
FR2933956A1 (en) | 2010-01-22 |
RU2011106025A (en) | 2012-08-27 |
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